Service difficulty report · Fitting · Cndair CL6002C10

Difficulty date
June 9, 2010
Submitted
June 11, 2010
Operation
Air carrier
Aircraft
N712EV
Make and model
Cndair CL6002C10
Aircraft serial
10074
Aircraft time
18,914 hours, 12,933 cycles
Engine
Ge CF348C1
Part
Fitting
Condition
Cracked
Location
Bulkhead
Stage of operation
IN
How discovered
E
Nature of condition
O
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

WHILE PERFORMING THE EDDY CURRENT OF THE RT BULKHEAD BATHTUB FITTING RECEIVED A RELAVANT CRACK INDICATION AROUND THE RETURN LINE OPENING. FINISHED DRILLING AND FINAL SIZED ALL FASTENER HOLES. APPLIED PRIMER & WET INSTALLED NEW FITTING. ABOVE WORK DONE REF SRM 51-42-21 AND REO PL670-53-61-034. REMOVED CRACKED BULKHEAD BATHTUB FITTING REF SRM 51-42-21. COMPLIED WITH EDDY CURRENT INSP OF ORIGINAL CUTLINE ON RT SIDE AFT PRESSURE BULKHEAD AT FS 1098 IAW NDTM 51-20-006, PART 1. NO DEFECTS NOTED AT THIS TIME. TRIMMED NEW FITTING, DRILLED NEW HOLES FOR HYD LINES & STARTED DRILLING NEW FASTENERS HOLES IAW SRM 51-40-00 AND REO 670-53-61-034. WORK DONE REF SRM 51-42-21 AND REO PL670-53-61-034.